US2947933A

US2947933A - Induction generator tachometer

Info

Publication number: US2947933A
Application number: US740291A
Authority: US
Inventors: Sidney A Davis
Original assignee: EASTERN AIR DEVICES Inc
Current assignee: EASTERN AIR DEVICES Inc
Priority date: 1958-06-06
Filing date: 1958-06-06
Publication date: 1960-08-02
Anticipated expiration: 1977-08-02

Description

Aug. 2, 1960 s. A. DAvls l 2,947,933

' INDUCTION'GENERATOR TAcHoMETER Filed June e, 1958 v l INVENToR t j F/ 6. 5 s//vfy A. amr/s ATTORNEYS United States INDUCTION GENERATOR TACHOMETER Sidney A. Davis, East Norwich, N.Y., assigner, by mesne assignments, to Eastern Air Devices, Inc., Dover, N .I-I., a corporation of Delaware Filed June`6, 1958, Ser. No. 740,291 19 Claims. (Cl. S22- 47) The present invention relates to the design of induction generator tachometers and the systems in which they are used in order to eliminate or minimize certain troublesome errors to which these devices are subject.

An induction generator tachometer is a device similar to atwo-'phase induction motor but in which only one of the phases is energized by alternating current. A Voltage is induced in the other winding the magnitude of which is determined by the speed of rotation of the rotor. A` generaldescription of this type of device and a fairly detailed analysis of the types of errors which are present in-such devices isv to be found in my article entitled Performance Characteristics of the Induction Generator Tachometer, published inthe January 1953 issue f Product Engineering.

Ideally no voltage shouldbe induced in the second winding when the rotor isstationary and the voltage induced in the second winding should be linearly proportional to the speed of rotation of the rotor. true linearity in the relationship between outpntvolta'ge and speed of rotor rotation does not obtain because of the leakage reactance and resistance of the primary or A.C. energized winding, and sometimes because of rotor leakage. Departure from linearity (non-linearity) represents 1an error which limits the useability of these devices.

This invention is directed primarily to the elimination or minimization of the non-linearity error in devices of this type, and, when desired, to the achievement of this result while at the same time producing an output which is at or close to the maximum value which can be obtained. According to one approach here disclosed, only the in-phase components of the output current are considered. This is permissible, since the quadrature errors can be compensated for or corrected in known ways independent with the teachings herein set forth. However, means are also here disclosed for eliminating non-linearity of the output with respect to rotor speed while at the same time preventing the occurrence of quadrature errors, and incertain instances this can even be accomplished at the Sametime that the magnitude of the output is maximized.

By a proper analysis of the circuitry involved in an induction generator tachometer, and by the properk design of that generator and the appropriate selection of circuit elements which can be incorporated thereinto or used in conjunction therewith, the errors of the type set forth above can be minimized or entirely eliminated. Moreover, these eifects can be obtained quite simply, without giving rise to any manufacturing problems, and without adding in any appreciable degree to the expense of the device or of the circuitry associated therewith.

The circuit analysis which follows will set forth certain relationships which should exist as regards various of the parts of the device in order to obtain the desired mini mization of the errors involved; These relationships can be satisfied either by simple modifications of the tachometer structure, generally involving the use of known ma terials in the rotor to produce an optimum value of rotor However,

resistance, or by the addition to the primary circuit of simple components (resistors or capacitors).

In accordance with the above, and to such. other objects as may hereinafter appear, the present invention relates to the design of induction generator tachometers and the systems in Whichthey are used, as dened in the appended claims and as described in this specification,

taken together with the accompanyingdrawings, in which:

Fig. 1 is an idealized cross sectional view of a drag-cup type of induction generator tachometer;

Fig. 2 is a schematic diagram' of an induction generator tachometer, the rotor being shown as of the squirrel cage type;

Fig. 3 is a complete equivalent circuit of an induction generator tachometer; y

Fig. 4 is a sirnplied equivalent circuit of a drag cupA wound. Positioned inside the stator 4 is a second mag-` n'etically permeable stator portion 8l The rotor lllv is constituted by a cup formed of appropriate conductive material to which shaft 12 is secured,` that shaft being rotatively journaled in the casing 2 as by means of the bearing 14. As may beV seen from reference to Fig. 2, the windings 6 are constituted by primary winding 6a and secondary Winding 6b disposed inquadrature relationship. The primary winding 6a is adapted to be energized by a suitable source of nat'ed V1. Under `normal conditions, with the rotor 10 stationary, no voltage will be induced in the secondary winding 6b. However, when the rotor 10 is rotated the moving rotor will cause a distortion of the flux within the generator so that some of that iiuX will become linked with the secondary winding 6b and generate an alternating voltage therein, designated V2. The degree of flux distortion will be determined by the speed at which the rotor lil is rotated, and thus the magnitudelof'the voltage V2 generated at the secondary winding 6b Will be determined by that speed of rotor rotation. In order for the voltage V2 to be an accurate measure of the Speed of rotor rotation it is desirable that it be accurately anddirectly proportional thereto, that is to say, that the voltage output V2 be accurately linearly related to the speed of rotation of the rotor 10. This is true Whether the rotory be of the drag cup type specically shown in Fig. l -or of the squirrel cage type schematically represented in Fig. 2.

Fig. 3 represents an equivalent circuit of an induction tachometer generator. In that circuit rS represents the resistance of the primary winding 6a, jXSI represents the leakage reactance of the primary winding, rm representsthe oo re loss, J'Xm represents the shunting impedance of the primary winding, jXlr represents the rotor leakage, rr represents theV equivalent rotor resistance, jXsl represents the leakage reactance of the secondary winding, rs represents the resistance of thesecondary Winding, v represents the ratio of the actual speed of to the synchronous speedvof rotation thereof, a represents the ratio of secondary effective turnsto primary effective turns and J represents circuitry to provide for a y degree phase shift. Thiscircuit maybe simplified to that shown in Fig. 4 by disregarding the rotor core loss rm. When drag cup type tachometrs arefinvolved this' simplification is entirely admissible, and no significant error in calculation vwill result, since those characteristics of the drag-cupdevice may'belconsidered negligible. When squirrel cage rotors are involved this alternatingv currentdesig-4 rotation Vof the rotorl leakage X1, and the 3 simplification may introduce an error, but the circuit analysis which follows, based upon the simplilied circuit diagram of Fig. 4, will nevertheless give rise to results with a squirrel cage rotor which, while not perfect, yare nevertheless superior to the results previously obtained without regard to these calculations, In Fig. 4 the circuit elements included within the box 16 constitute the rotor of the device, and the symbols .Zp and Zs represent the impedances of the primary and secondary windings 6a and 6b respectively.

The circuit elements shown in IFig. 4 may be represented on a dimensionless basis, the various symbolsl for this dimensionless analysis being shown on Fig. 4 in parenthesis. T, representing the dimensionless primary or secondary leakage impedance, equallng Tr+jTx (where PF-) and CPF-l for the primary winding). a represents the dimensionless cup resistance and is equal to If. X m

The apparent rotor input impedance, as viewed looking to the right from points A, B in Fig. 4, is

It will be noted that both the apparent input impedance and the total primary shunt impedance are dependent upon v, which is determined by the speed of rotation of the rotor. Since the impedance looking into the rotor circuit will therefore normally vary with the speed of the rotor rotation, it follows that under ordinary circumstances the tachometer will tend to draw a variable current as its speed increases. 'I'his variable current passing through the leakage impedance of the primary will cause a voltage drop which will also vary with rotor speed, thereby changing the voltage across the shunting air gap reactance of the primary. Thus variation of speed gives rise to that non-linearity of voltage output with speed which it is the objective of the present invention to eliminate.

The gain K of the primary `and rotor circuits, that is to say, the relationship between the voltage across the points A, B and the voltage V1 in Fig. 4, may be represented as follows:

Substituting for Tp the appropriate values of Tr and TX, this relationship in turn may be expressed as follows:

If D is squared (as I prefer to do for simplification of calculation), and disregarding phase, since we are at this point interested only in the magnitude errors, the following relationship results:

respectively except for those elements which include v, then D2= (w+ Trv2 2+ (1f-l- Trvz)2 (8) Differentiating D2 with respect to v2 we get:

2 %=2o+ lava T.+2 s+ uw) T. 9)

If now this differentiation is set equal to zero and is solved, we get:

IIf we now let V=0, which is an admissible working hypothesis, since all good tachometers are designed -for operation as speeds far below synchronous speed', Equation l0 reduces to:

Substituting the initial values for 'y and the following relationship is obtained:

This relationship is one which will, insofar as the magnitude of lthe output is concerned, and disregarding quadrature errors, give rise to a mode of operation in which the voltage output V2 is directly and linearly proportional to the speed of rotor rotation.

It will be noted that there are three variables in that relationship, to wit, Tr, Tx and a. Tr and TX Vcan be varied by connecting appropriate resistors or capacitors in series with the primary winding 6a, the addition of a resistor increasing the value of Tr and the addition of a capacitor decreasing the value of TX. The other variable, a, is determined by the resistive value of the rotor, and

may also be varied through the choice of appropriatematerials therefor.

It is also possible to eliminate magnitude non-linearity while at the same time obtaining substantially maximum output from the secondary winding 6b. It can be shown that maximum tachorneter output occurs when ot=l, from the following reasoning: The tachometer voltage gradient is proportional to the torque/watt of the unit used as a motor. The equivalent circuit for one phase of the unit used as a motor, at low speeds relative to synchronous speed (which is the usual condition at which these generators are operated) is set forth in Fig. 5. Assuming a given current input I to the circuit of Fig. 5, the current in a is l then it follows that the non-linearity effect will be eliminated if that relationship is satisfied.

the power in a is Iza l-l-ct2 The denominator, D, of K may be expressed as folthe power in Tr is 12Tr and thus the total powerY is The conventional copper-manganese alloy usually used for the drag cups gives rise to an a of 2.5, but an a of 1 can beachievediin many instances by forming the cup 10 of an aluminum alloy.

For the special case wherevrx=lfrelationship (12) for eliminating in-phase linearity error simplifies to the very simpleV relationship:

TrzTx If phase shift errors are not to beignored, `itlisknown that'a zero phase shift error'is obtained vvhentheV fol-y lowing relationship exists:

a TrT-ZZ-i-TX) (14) This relationship, as well as relationship (12) for linearity of the in-phase signal, can be simultaneously achieved if T, =(l. In such a case Tx may bebrought to zero by connecting a capacitor of appropriate value in series with the primarywinding 6a, and, for a' given a, Tr may be'brought to its desired value by connecting a resistance in series with the primary winding 6a.

It will be seenl from the above that in the special case:

where a=l (which, as has been shown,visthe condition for maximum in-phase output) If, in'addition, T ,4:0, all three'of the desired resultslinearity of output, zerophase'shift, and maximum output-are simultaneously obtained. This situation can be brought about by driving the primary winding 6a from an` infinite impedance source. There are many known ways in which that can be done. The primary winding 6a can be connected for push pull operation driven by anamplifier havingV a twin pentode output stage and having precise gain. yA very large dropping resistor can be interposed between the energizing source and the primary winding, which resistor will consume much more power than will the tachometer. An amplifier employing, current feedback could bev usedv to energize the prmary winding 6a, such anamplitier giving an output current proportional to input voltage and therefore'acting like a very high impedance current source. This exposition is merely exemplary, and many modes of achieving this result will be apparent.

From the above analysis it will beseen that a series of novel relationships have been developed to achieve the desiredresult's.y These may be designated as-A, B, C and D and are as follows:

-General expression for.` elimination of in-phase nonlinearity: Y Y

B-In-phase non-linearity eliminatedand maximum inphase output obtained:

D--In-phase non-linearity. eliminated, phasel shift error eliminated, and maximum in-phase output obtained:

rThe above analysis represents an approach tothe problem' of-V eliminating errors in devices ofy the. typeunder discussion inY which the various errors are balanced againstoneanother insuch` a manner as to produce 'the desiredfendresult.` This contrasts-With the conventional v approach which' attempts to minimize each of the error components individually.-

Considering relationshipA, it will be seen that for. a

variety of values for a (which is determined by the rotor resistance) there are corresponding sets of values of the leakage impedance parameters which will give the desired condition. In some cases Tg, the reactive portion of the leakage impedance, may have to ybe negative. This can be achieved by using a capacitor of appropriate magnitude in series with the primaryy winding 6a'. In some instances Tr, the resistive portion of the leakage impedance, may have to be negative. This result can ba achieved by driving the primary winding 6a through an electronic amplifier.

To illustrate the manner in which these relationships may be achieved, a few specific examples are set forth. A drag cup induction generatorr tachometer, as manufactured for 400 cps.v operation, may have a primary winding resistance rs of 100 ohms, av primary winding leakage reactance X51 of 100 ohms, a primary winding shunting impedance Xm of 400 ohms, and an equivalent drag cup resistance rr of lOOOvohms. As a result T,=%, rrr-.1a and =2.5.

With this particular example, in which Tr already equals TX, non-linearity can be eliminated and-maximum output simultaneously obtained merely by changing a from 2.5 to l. One way in which this can be accomplished is by utilizing an aluminum alloy for the drag cup 10.

If the tachometer orignallyhad had a primary leakage reactance X51 of 20() ohms, the necessary equality between Tr and Tx could'be obtained (once a has been brought to the value of l), either by increasing T, by adding an additional 100 ohm resistance in series with the primary winding 6a or by reducing Tx by connecting a 4 mfd. capacitor in series with the primary winding 6a, such a capacitor having a negative reactance at 400 c.p.s. of l0() ohms.

If zero phase shift error is of importance, and with a drag cup 10 formed of a copper manganese alloy so that a=2.5, zero phase shift error and non-linearity can both be eliminated by connecting a 4 mfd. capacitor in series with the primary winding. 6a, thus making TX=O. Substituting a value of 2.5 into the equation for Trfwe lind that T1F should equal .477. Resistance is then added f in series with the primary winding 6a so that the sum of the winding resistance and the added resistance equals 190.8 ohms (.477 400).

By the novel approach to the design of induction ta-v chomcters as :above set forth it is seen thatsevenal of the most troublesome errors to which these devices are subject can be eliminated through proper design off the units and of thesystemsl in which theyare employedrso that the relationships aboveset forthwill obtain. This can bedone in van uncomplicatedvand reliable manner; For linearity theconnection vofa resistorlor oap'acitoriof appropriate value in series with the primary winding 6a will achieve the desired result. For maximum output the internal design of the rotor can be modified, as through the use of appropriate-materials. Zero phase shift error and linearity can be simultaneously obtained in many cases, and maximum output can lalso be obtained at the same time through the use of appropriate driving circuitry.

When the Iabofve teachings are carried out the operation of the tachometer with the specified errors eliminated or minimized is not particularly temperature sensitive, and the desired results will be obtained over a band of temperatures in the vicinity of the nominal temperature at which the parameters are set. This is satisfactory in many installations. Insensitivity to temperature changes is particularly marked when a=1. rIhe same situation obtains with respect to sensitivity to small changes in the frequency of the energizing current. Indeed, when a series capacitor Iis included in the primary circuit for the purposes above set forth, a greater degree of insensitivity to line frequency variation is obtained than would otherwise be the case. Thus carrying out my teachings through the use of such a ser-ies capacitor has this a'rlditional desirable effect.

While but a few specific embodiments of the present invention have been set forth above, it will be apparent that my invention is not limited thereto, but is of a general and broad nature as defined in the following claims.

I claim:

1. An induction tachometer comprising a primary circuit, a secondary circuit, and a rotor operatively connected to said circuits, in which the following relationships exist: l

a representing the ratio between the rotor resistance and the shunting impedance of the primary circuit, and Tr and Tx representing the ratios between the resistance and reactance respectively of the pnimary circuit as numerator and the shunting `impedance of the primary circuit as denominator.

2. An induction tachometer comprising a primary circuit, a secondary circuit, and a rotor operatively connected to said circuits, in which the following relationships exist:

a=l and' TrzTx a representing the ratio between the rotor resistance and the shunting impedance of the primary circuit, Tr and Tx representing the ratios between the resistance and reactance respectively of the primary circuit as numerator and the shunting impedance of the primary circuit as denominator.

3. An induction tachometer comprising a primary circuit, a secondary circuit, and a rotor operatively connected to said circuits, in which the following relationships exist:

a representing the ratio between the rotor resistance and the shunting impedance of the primary'circuit, T, and TX representing the ratios between the resistance and reactance respectively of the primary circuit as numerator and the shunting impedance of the denominator.

5. An induction tacohmeter comprising a primary circuit, a secondary circuit, and a rotor operatively connected to said circuits, Iin which the following relationships exist:

a representing the natio between the rotor resistance and the shunting impedance of the primary circuit, Tx representing the ratio between the reactance of the primary a representing the ratio between the rotor resistance and the shunting impedance of the primary circuit, Tx representing the ratio between the reactance of the primary circuit yand the shunting impedance of the primary oircuit, in combi-nation with a driving source connected to said primary circuitl and effective to provide a primary equalling Tx.

current proportional to the voltage input to said source.

7. An induction tachometer system comprising a primary winding, a secondary winding, and a rotor operatively connected to said windings, in which a represents the ratio between the rotor resistance and the shunting impedance of the primary winding, and in which an impedance is connected with said primary winding, said impedance having a value such, with relation to the values of the resistance and reactance of the primary winding, as to cause the following relationship to exist:

Tr and TX representing the ratios between the resistance and reactance respectively of the primary winding as numerator and thel shunting impedance of the primary winding as denominator.

8. The system of claim 7, in which azl, Tr therefore 9. The system of claim 8, in which said impedance comprises a resistor connected in series with said primary winding, thereby to increase the value of Tr.

10. The system of claim 8, in which said impedance comprises a capacitor connected in series with said primary winding, thereby to decrease the value of TX.

ll. The system of claim 7, in which said impedance comprises a resistor connected in series with said primary winding, thereby/.to increase the value of T1..

12. The system of claim 7, in which said impedance comprises a capacitor connected in .series with said primary winding, thereby to decrease the value of TX.

13. An induction tachometer system comprising a primary winding, a secondary winding, and a rotor operatively connected to said windings, in which a represents the ratio between the rotor resistance and the shunting impedance of the primary Winding, and in which an impedance is connected with said primary winding, said impedance having a value such, with relation to the values of the resistance and reactance of the primary winding, as to cause the following relationships to exist:

TX=G and Tr:

primary circuit yas 15. The system of claim 13, in which said impedance comprises a capacitor connected in series with said primary winding, thereby to decrease the value of Tx.

16. An induction tachometer system comprising a primary winding, a secondary winding, and a rotor opera- .tively connected to said windings, in which a represents the ratio between the rotor resistance and the shunting impedance of the primary winding, and in which an impedance is connected with'said primary Winding, said impedance having a value such, with relation to the values of the resistance and reactance of the primary winding, as to cause the following relationships to exist:

said primary winding being connected to an input circuit, the ratio of the combined resistance of the primary winding and its input circuit to the shunting impedance of the primary winding being substantially infinite in value.

17. The system of claim 16, in which said impedance comprises a capacitor connected in series with said pri mary winding, thereby to decrease the value of Tx.

18. An induction tachometer system comprising a primary winding, a secondary winding, and a rotor operasaid primary winding being connected to a driving source, said source providing a driving current to said primary winding proportional to the voltage input to said driving source.

19. The system of claim 18, in which said impedance comprises a capacitor connected in series with said primary winding, thereby to decrease the value of Tx.

References Citedl in the file of this patent UNITED STATES PATENTS Schroeder May 16, 1950 Hansell Feb. 6, 1951